Defence NSN Source is a one-stop shop for Damper Turbine Blade Aircraft Tu components and other similar products that meet the needs of our customer base. You have taken a specific interest in part number 4082885, a United Technologies Corporation offering we carry that is listed alongside the NSN 2840-01-440-1697 to streamline identification and procurement. If you fill out and submit the Request for Quote (RFQ) form located below, you can secure pricing options for your comparisons. Within 15 minutes of one of our team members receiving and reviewing your submission, you can anticipate a customized response.
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We strive to make the procurement process more straightforward and efficient by offering comprehensive details for listed components whenever possible. For instance, part number 4082885 was manufactured by United Technologies Corporation under the CAGECode 77445. Moreover, by using the first digits of the NSN 2840-01-440-1697, we can see that this product belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Utilizing such information, you can ensure that you are securing precisely what you need to carry out operations or meet your project requirements. Keeping this in mind, obtain a quote on part number 4082885 with our online services.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-440-1697 Item PartTypeName: DAMPER,TURBINE BLADE,AIRCRAFT TU | 2840 | 014401697 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4082885 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 0.565 INCHES MINIMUM AND 0.571 INCHES MAXIMUM |
| ABMZ | DIAMETER | 16.788 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CQFM | HARDNESS RATING | 34.0 ROCKWELL C MINIMUM OVERALL AND 44.0 ROCKWELL C MAXIMUM OVERALL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 21; REPL P/N 4074864 ONCE TCTO HAS BEEN ACCOMPLISHED; RETAINING PLATE DAMPER IS SYMMETRICAL IN SHAPE AND HAS 6 RETENTION TABS FORWARD AND AFT TO PRECLUDE POSSIBLE REVERSE INSTALLATION AND RESULTING CUT-OFF OF CO |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
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